Vertical lift control system

Abstract

The invention disclose a vertical lift control system, a plane body comprises a lifting cord system, a skeleton and a lower bracket, the skeleton comprises a control board, a power source and a main skeleton, the main skeleton comprises a upper part of the main skeleton, a lower part of the main skeleton, a hollow cavity made by the lower part of the main skeleton and a main frame, the control board is eclectically connected with the power source and is taken in the hollow cavity, compared with the prior art, the vertical lift control system adapts a main, auxiliary propeller structure which can rotate in the opposite direction mutually, in this way, the instability of the vertical and lift control system by unidirectional power is overcome.

Description

technical field [0001] The invention relates to an electric toy, in particular to a vertical lift aircraft. Background technique [0002] The vertical lift control system has been loved by people since it came out. In order to meet the needs of consumers, toy manufacturers continue to develop various vertical lift control system models and make continuous improvements in order to create a vertical lift control system that can fly stably and is easy to control. system. At present, the vertical lift control system on the market generally has the problem of unstable flight and is not easy to operate. The main reason for the unstable flight is that the propeller produces a one-way force from rest to rotation during flight, which makes the vertical lift control system unable to maintain the vertical lift control system during flight. Balanced state, thus making the flight unstable. It is not suitable for operation because the steering mechanism of the vertical lift control syst...

AI Technical Summary

Problems solved by technology

At present, the vertical lift control system on the market generally has the problem of unstable flight and is not easy to operate. The main reason for the unstable flight is that the propeller produces a one-way force from rest to rotation during flight, which makes the vertical lift control system unable to maintain the vertical lift control system during flight. Balanced state, thus making the flight unstable

It is not suitable for operation because the steering mechanism of the vertical lift control system currently on the market mostly adopts the tail steering structure, and the steering control part and the flight control part are not together, which makes the operation more difficult

[0003] In addition, the lower bracket of the vertical lift control system currently on the market is mainly a tripod structure without rollers. The biggest disadvantage of this structure is that it is poor in safety.

When the vertical lift control system lands, there is often a large forward momentum, and because the vertical lift control system does not always land perpendicular to the ground, the lower bracket is likely to cause the vertical lift control system to fall due to the lack of rollers

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